Integrated Fluid — Structure Simulation for Full Burning of a Solid-Propellant Rocket Interior
Influence of Fe2O3 Size on Burning Characteristics of Ammonium Nitrate/ Fe2O3 Propellants
Suppressing a High-Frequency Instability with Varying Bands of White Noise
Surface Instability on Cryogenic Swirl Flow at Sub- to Supercritical Conditions
Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors
SURVEY PAPERS - Review of Worldwide Activities in Liquid-Fed Pulsed Plasma Thruster
Platinum/Barium Hexaaluminate Catalyst to Small-Scale Hydroxylamine Nitrate Thrusters Application
Powerplant Design and Performance Analysis of a Manned All-Electric Helicopter
Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers
Prediction of Combustion Noise for an Aeroengine Combustor
Demonstration of Compact Air Separation Technology for In-Flight Oxygen Collection Space Launchers
Mechanistic Assessment of Swirl Coaxial Injection by Quantitative X-Ray Radiography
Power Deposition into the Discharge Channel of a Hall Effect Thruster
Experimental and Numerical Multiphase-Front Fluid Hammer
Reactive, Mechanically Alloyed Al . Mg Powders with Customized Particle Sizes and Compositions
Increasing Reliability of a Two-Stroke Internal Combustion Engine for Dynamically Changing Altitudes